Part #:
Model: KC-192
NSN: |
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OEM: |
BendixKing |
Desc: |
Autopilot Computer |
Select part number above to view pricing and availability.
| Price | Condition | Status | More Info | |
|---|---|---|---|---|
| $5,950.00 | SV OUTRIGHT | 2 IN STOCK | VIEW | |
| $2,995.00 | SV EXCHANGE | 2 IN STOCK | VIEW |
| Price | Condition | Status | More Info | |
|---|---|---|---|---|
| $12,500.00 | SV OUTRIGHT | REQUEST LEAD TIME |
|
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| $3,750.00 | SV EXCHANGE | REQUEST LEAD TIME |
|
KC-192
- Mode Controller / Flight Computer / Annunciator
- Flight Computer for the KFC-150 Autopilot System
- Incorporates all computer functions, mode control buttons & annunciator lights in a single unit
- Panel Mount
- Annunciates all vertical & lateral flight director & autopilot system modes
- Contains altitude sensor
- Has 7 push buttons for engaging flight director and/or autopilot modes, a push button to initiate a system self-test, and a vertical trim rocker switch to allow for changing the aircraft's pitch up or down without disconnecting the autopilot
- Certified in over 40 different aircraft types
- Connector modules are used to adapt the computer software to preform satisfactory with each individual airframe - connector modules are sold & shipped separately
- A self test is required before autopilot engagement is allowed
- Interfaces with the KS-17X and KS-27X series of servo actuators
SPECIFICATIONS
| Size: | 6.312" w x 1.55" h x 11.62" L | Weight: | 2.6 lbs max (unit only) |
| Temperature: | -20°C to +55°C | Altitude Range: | Up to 35,000 ft |
| Power Input: | +28VDC @ 1.2A, 14VDC @ 2.4A | Power Output: | +15VDC @ .2A -15VDC @ .2A +5VDC @ .2A 10VAC 506 Hz @ 2.5 VA |
| Vertical Reference: | 2 Wire, Pitch & Roll, 206mVAC per degree; 2 Wire, Pitch & Roll, 206mVAC per degree (EFIS) | Directional Reference: | 2 Wire Heading Datum, 550mVDC/Degree; 2 Wire Heading Datum, 393mVAC/Degree (EFIS) |
| Course Datum: | 2 Wire Course Datum, 210mVDC/Degree; 2 Wire Heading Datum, 393mVAC/Degree (EFIS) | VOR/RNAV Receiver: | 60mV/Deg/Localizer, 15mV per Deg/VOR, 30mV/NM RNAV Enroute, 120mV/NM RNAV APPR |
| LOC Energize Sense: | Ground for LOC Enable | Glideslope Receiver: | 214mV/Deg |
| Symbol Generator (EFIS) Valid: | 0/28V, 1 Wire | Glideslope Valid: | 180mV for Valid |
| Middle Maker Sense: | 1 Wire, 2VDC Min for MKR on | Outer Marker Sense: | 1 Wire, 2VDC Min for MKR on |
| Pitch Servo Tach Feedback: | 2 Wire, DC Differential voltage | Roll Servo Tach Feedback: | 2 Wire, DC Differential voltage |
| Switched 28VDC: | 1 Wire | Yaw Damp Engage: | 1 Wire |
| Compass Valid: | Hi = Invalid, Ground = Valid; 28V = Valid, Ground = Invalid (EFIS) | Back Lighting: | 3 wires (14 or 28V inputs) |
| Pitch Servo Drive: | 2 Wire DC Differential, 0 to 28V max | Roll Servo Drive: | 2 Wire DC Differential, 0 to 28V max |
| Servo Clutch Engages: | 1 Wire, 14V or 28V to engage | AP Valid:> | Open = Valid, Ground = Invalid |
| VG Excitation: | 10VAC @ 506Hz | Pre-Flight Test Out: | 1 Wire 28V = Test Mode On |
| External Annunciation: | 7 wires |
| Part Number: | Description: |
|---|---|
| 065-0042-00 | Autopilot Computer, 14 volt - obsoleted |
| 065-0042-01 | Autopilot Computer. 28 volt - obsoleted |
| 065-0042-02 | Autopilot Computer, 14 volt - standard |
| 065-0042-03 | Autopilot Computer, 28 volt - standard |
| 065-0042-04 | Autopilot Computer, 14 volt - With G-Dump |
| 065-0042-05 | Autopilot Computer, 28 volt - With G-Dump |
| 065-0042-06 | Autopilot Computer, 14 volt - With Improved G-Dump |
| 065-0042-07 | Autopilot Computer, 28 volt - With Improved G-Dump |
| 065-0042-09 | Autopilot Computer, 28 volt - For Lake Renegade |
| 065-0042-12 | Autopilot Computer, 28 volt - With Lightning Resistance |
| 065-0042-15 | REPLACES all Flavors |
| 065-0042-16 | For EFIS Installations |
| Price | Condition | Status |
|---|---|---|
| $5,950.00 | SV OUTRIGHT | 2 IN STOCK |
| $2,995.00 | SV EXCHANGE | 2 IN STOCK |
| Price | Condition | Status |
|---|---|---|
| $12,500.00 | SV OUTRIGHT | REQUEST LEAD TIME |
| $3,750.00 | SV EXCHANGE | REQUEST LEAD TIME |
Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com
Why do some parts indicate "REQUEST" or “RFQ” on the Southeast Aerospace website?
In relation to NE (New) parts, many OEMs change their prices and availability without any notice to dealers or the industry. Therefore, through the REQUEST or RFQ indication, we ask that customers contact us for the most accurate price and availability.
In relation to SV & OH parts, the used parts aftermarket in the aviation industry is not an infinite supply. It is a dynamic, constantly changing market that is significantly affected by and susceptible to highs and lows in supply and demand. Therefore, although we attempt to, at times, we are unable to predict the exact moment when an item may be available. Once again, through the REQUEST or RFQ indication on our website, we ask that customers contact us for the most current and accurate price and availability.
Why is Service Bulletin 11 for the KI-256 required in some autopilot installations?
Service bulletin 11 for the KI-256 reduces loading effects to the autopilot pitch and roll outputs. It is required in most installations where the KI-256 is used with the KC-192 autopilot computer Part Number 065-0042-15.
What is the difference between Honeywell (Bendix/King) part numbers with 9 digits vs. 12 digits?
Why did Bendix/King change their part numbers from a 9 digit to a 12 digit format?
Different software versions imply different operational features and/or interface capabilities and software modifications imply software repairs (bug fixes) to insure proper operation of these features and interfaces. Software version upgrades frequently require hardware modifications to the unit. Such hardware modifications accompanying software version upgrades do not necessarily change the hardware version of the unit.
The KC-192 I just received does not seem to be working, what could be the cause?
Are SEA's Exchange prices negotiable?
Negotiating the exchange price of a unit only limits the allowable repair cap for the core unit. Southeast Aerospace's exchange transactions are based on the return of economically repairable core unit. Once the core is received and evaluated, the core repair cost incurred by SEA cannot exceed 75% of the original exchange price. That is, it cannot cost SEA more than 75% of the original OH/SV exchange price collected from the customer. Therefore, when and if an SEA exchange price is discounted, there is a risk that additional charges may be assessed once the core is returned and evaluated.
Is there anything that can replace my original KC-192?
According to Honeywell Installation Bulletin 385, KC-192 Part Number 065-0042-15 a direct replacement for any of the following part numbers:
| 065-0042-00 | 065-0042-05 |
| 065-0042-01 | 065-0042-06 |
| 065-0042-02 | 065-0042-07 |
| 065-0042-03 | 065-0042-09 |
| 065-0042-04 | 065-0042-12 |
The adapter modules used in the aircraft configuration have not been changed and function exactly the same exactly the same with the -15 computers. Click Here to download the Installation Bulletin.
When using the updated KC-192 -15 computer, check the mod status of the KI-256. If the KI-256 does not have Mod 11, then you may encounter alignment issues with the updated KC-192. Therefore, it is highly suggested (and necessary in some cases) to incorporate Mod 11 into the KI-256. KI-256 Service Bulletin 11 updates a PC board in the indicator that reduces loading effects to the pitch and roll outputs. The cost to incorporate Service Bulletin into the KI-256 is approximately $1000.
Is there anything that will directly replace the KC-191 and KC-192 autopilot computers?
No, there are not different model computers that will replace the KC-191 or KC-192 computers. However, the -15 version of each computer replaces older, existing part numbers for each computer. Please refer to Honeywell Installation Bulletin No. 385 for reference.
What are the adapter modules for the KC-192?
